US1929566A - Airplane - Google Patents

Description

061;. 10, 1933. SANDERS 1,929,566

AIRPLANE Filed March 30, 1931 2 Sheets-Sheet l INVENTOR Luowls A. SANDERS ATTORNEY Oct 10, 1933. A. SANDERS 1,929,566

AIRPLANE Filed March 30, 1931 2 Sheets-Sheet 2 INVENTOR L uowm A.5ANDER5 ATTORA/E Y Patented Oct. 16, 1933 AIRPLANE Ludwig Adrian Sanders, Voorburg, Netherlands; assignor to Johann Anton Sanders, Voorburg,

Netherlands, and Frans Hague, Netherlands Application March 30, 1931, Serial No. and in the Netherlands April 7, 1930 Lambert Stoot, The

4 Claims. (Cl. 244-12) from Fig. 1. In this embodiment the upper surfaces of the wings are shaped according to the said parabolas, the lower surfaces not. How- The invention relates to an airplane in which the wing and the body gradually merge into each other and all sections, parallel to the main symmetry plane, are profiles having the same shape of profiles gradually decreasing towards the ends of the wing.

According to the invention the wings is decreasing parabolically towards the end in such a way that the top of the parab- 01a is located near the root of the wing. In

. other words, the top surface of the wing curves parabolically to correspond to a parabola, the

directrix of which is horizontal and the vertex or top of which is located near the root of the wing.

Also according to the invention the sections of the wing may be so displaced mutually that their chords are no longer parallel to the chord of the main symmetry surface.

The most important advantage of the invention is this that in this way the 'most, favourable configuration of the longitudinal girders as regards their structural height is obtained, and at the same time the wings in plan view will approach the most ideal shape, confined by parabolas, whereby the supporting effect of the wings is most favourable. Thereby an airplane constructed according to the invention has a larger radius of action than other airplanes, because the resistance is reduced to a minimum.

The construction is extremely simple, because the complete plan of the whole airplane is determined by the front View and a normal profile. fhe thickness of the wing therefore is the starting detail. The shape of the wings in plan view will become such that the bounding lines of the same are also parabolas tops near the root of the wings.

Some embodiments of the invention are illustrated in the accompanying drawings.

Fig. 1 is a front View and Fig. 2 a top view of one of the embodiments.

Fig. 3 is a sectional View wing of Fig. 2.

Fig. 4 is a front View and Fig. 5 a top view of a second embodiment.

Fig. 6 is a front view and Fig. 7 a top view of a third embodiment.

In all embodiments all sections, parallel to the main symmetry plane, such as shown in Fig. 3, are unform profiles.

The thickness of the wings 2 is decreasing gradually towards the ends, of the wings, according to a parabola, the top of which is located near the root of the wing. This appears taken through the t the thickness ofsaid parabola having their ever, it is just as well possible lower to construct the surfaces according to such a parabola and the upper surfacesnot, or to form both surfaces parabolically, but always according to a parabola the top of which is root of the wing.

located near the In Fig'. 1 and lines 8, 9, 10 and 11 indicate the thickness of the wing at four wing. These lines are erected vertically on the lower surface and of such a length that their tops are confined by the parabola 12, the top of which is located near the root of the The same is seen at the other wing. The p is indicated there by 14 and the topby 15.

It appears from view, has been determined, the the airplane is determined by wing the above that if the front whole shape of the same.

parabola 12 crosses the lower surface 16 in the point 1'7 by which the length wings will not end in are finished as fixed. In practice the an acute point, but their ends indicated at 18 in Fig. 2. 7

According to the invention rious form may be constructed able to the special purposes for A few examples are given in the Figs. 4 and 5, and in'the Figs. 6 and 7.

In the embodiment of the Figs.

2 deviate in backward direction, the emintended.

wings of the wing is which are suitwhich they are bodiment of the Figs. 6 and Tshowing a double bodyl and being intended for a traffic-airplane.

places in the I airplanes of va- 4 and 5 the The embodiment of the Figs. 4' and 5 is suitable for pursuit-planes, e. g. for military purposes.

An airplane constructed according to the invention fully satisfies all aerodynamical requirements.

In view of the desired landing speed the sections of the supporting surfaces may be displaced gradually with regard to each other, so

that the chords of the sections are no longer symmetry surface.

parallel to those of the main I claim: 1. An airplane comprising a structed that the diiference body and wings, the thickness of the wings decreasing parabolically toward the ends, each wing being so conin thickness of abcla, the vertex of which lies at the root of the wing andthe' directrix of which is sui'istantially longitudinal;

2. An airplane comprising a body and wings,

the wing surface and the body merging into each other, said wings being so formed that all sec tions parallel to the main symmetry surface are uniform profiles having the same shape and decreasing gradually toward the ends of the wings, the thickness of the wings decreasing parabolically toward the ends, said wings being so constructed that a curve drawn through the upper extremities of the projections on a vertical plane of lines representing the vertical thickness of progressive adjacent sections of the wings parallel to the lateral axis of the craft is a parabola having its vertex lying at the root of the wings and its directrix substantially horizontal.

3. An airplane, wherein the wing surface and the body merge into each other, and all sections parallel to the main symmetry surface are uniform profiles having the same shape and decreasing gradually toward they end of the wing, the thickness of the wing decreasing parabolical- 1y toward the end in such a way that the vertex of the parabola in projection on a vertical plane parallel to the lateral axis of the airplane is located near the root of the wing and the directrix of which is substantially horizontal.

4. The airplane set forth in claim 1, wherein the sections of the wing are displaced gradually relative to one another so that the chords of the sections are no longer parallel to the chord of the main symmetry surface thereof.

LUDWIG ADRIAN SANDERS.

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